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Volumn , Issue , 1999, Pages 1-12

Cold-flow simulation and CFD modeling of the space shuttle solid rocket motor nozzle joints

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC PROPERTIES; CALORIMETERS; COMPRESSIBILITY OF GASES; COMPUTATIONAL FLUID DYNAMICS; FLOW OF GASES; GASES; HEAT FLUX; HEAT TRANSFER; PARALLEL FLOW; PROPULSION; ROCKET ENGINES; ROCKET NOZZLES; ROCKETS; SPACE SHUTTLES; THERMOCOUPLES;

EID: 84963877627     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-2793     Document Type: Conference Paper
Times cited : (5)

References (8)
  • 1
    • 0017452472 scopus 로고
    • Prediction of heat transfer under an axisymmetric laminar impinging jet
    • Sadd, N.R., Douglas, W.J.M, and Mujumdar, A.S. 1977 “Prediction of heat transfer under an axisymmetric laminar impinging jet,” Ind. Eng. Chem., Fundam., Vol. 16, pp. 148-154.
    • (1977) Ind. Eng. Chem., Fundam , vol.16 , pp. 148-154
    • Sadd, N.R.1    Douglas, W.J.M.2    Mujumdar, A.S.3
  • 2
    • 84982319076 scopus 로고    scopus 로고
    • Computation of jet impingement heat transfer by an adaptive finite element algorithm
    • Paper 98-2585
    • Turgeon, E. and Pelletier, D. 1998 “Computation of jet impingement heat transfer by an adaptive finite element algorithm,” AIAA Paper 98-2585.
    • (1998) AIAA
    • Turgeon, E.1    Pelletier, D.2
  • 3
  • 4
    • 0014700544 scopus 로고
    • Mass transfer in a non uniform impinging jet, Part 1 & 2
    • Scholtz, M.T. and Trass, O. 1970 “Mass transfer in a non uniform impinging jet, Part 1 & 2,” AIChE J., Vol. 16, pp. 82-96.
    • (1970) Aiche J , vol.16 , pp. 82-96
    • Scholtz, M.T.1    Trass, O.2
  • 5
    • 28844508053 scopus 로고    scopus 로고
    • Users Guide, Tutorials, FLUENT Inc, Lebanon, NH
    • FLUENT Inc, 1998, Users Guide, Tutorials, FLUENT Inc, Lebanon, NH.
    • (1998) FLUENT Inc
  • 6
    • 85085846714 scopus 로고
    • Computation of viscous chemically reacting flows in hybrid rocket motors using an upwind LU-SSOR scheme
    • paper 90-1570
    • Loh, H.T. and Golafshani, M. 1990 “Computation of viscous chemically reacting flows in hybrid rocket motors using an upwind LU-SSOR scheme,” AIAA paper 90-1570.
    • (1990) AIAA
    • Loh, H.T.1    Golafshani, M.2
  • 8
    • 84961960690 scopus 로고    scopus 로고
    • Evaluation of aft skirt length effects on rocket motor base heat using computational fluid dynamics
    • paper 962645
    • Loh, H.T., Smith-Kent, R., Perkins, F., and Chwalowski, P. 1996 “Evaluation of aft skirt length effects on rocket motor base heat using computational fluid dynamics,” AIAA paper 962645.
    • (1996) AIAA
    • Loh, H.T.1    Smith-Kent, R.2    Perkins, F.3    Chwalowski, P.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.